ClassID:

140340

F02K1/42 - CPC Classification

Classification description:

Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto; Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet the means being movable into an inoperative position

Recent Application in this class:
#1
20220268236
2022-08-25

Supersonic aircraft and method of reducing sonic booms and jet noise

#2
20200325849
2020-10-15

Dual function cascade integrated variable area fan nozzle and thrust reverser

#3
20200191156
2020-06-18

Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct

#4
20180291837
2018-10-11

Exhaust nozzle control including tapered control effector for a gas turbine engine

#5
20170356387
2017-12-14

Dual function cascade integrated variable area fan nozzle and thrust reverser

#6
20160377026
2016-12-29

Exhaust nozzle control for a gas turbine engine

#7
20160222917
2016-08-04

Nacelle for an aircraft engine with variable section nozzle

#8
20150121840
2015-05-07

Aircraft nozzle system

#9
20140030057
2014-01-30

AFT cascade translating variable area fan nozzle

#10
20130202404
2013-08-08

Methods and apparatus for deployable swirl vanes

#11
20120291415
2012-11-22

Dual function cascade integrated variable area fan nozzle and thrust reverser

#12
20120056005
2012-03-08

SHAPE MEMORY MATERIAL ACTUATION

#13
20100254803
2010-10-07

Turbofan engine noise suppression using fan flow deflector

#14
20100170220
2010-07-08

Turbofan engine having inner fixed structure including ducted passages

#15
20100089030
2010-04-15

CONTROLLING THE AERODYNAMIC DRAG OF A GAS TURBINE ENGINE DURING A SHUTDOWN STATE

#16
20100043393
2010-02-25

Gas turbine engine with variable area fan nozzle

#17
20100008764
2010-01-14

Gas turbine engine with a variable exit area fan nozzle, nacelle assembly of such a engine, and corresponding operating method

#18
20100005777
2010-01-14

Dual function cascade integrated variable area fan nozzle and thrust reverser

#19
20080286094
2008-11-20

Variable geometry nacelle assembly for a gas turbine engine

#20
20080022651
2008-01-31

Jet engine noise suppressor

#21
20070235080
2007-10-11

Adjustment assembly

#22
20070107414
2007-05-17

Jet engine noise suppressor

#23
20060000211
2006-01-05

Shape memory material actuation

#24
20050229585
2005-10-20

Gas turbine engine exhaust nozzle

#25
20050166575
2005-08-04

Gas turbine engine exhaust nozzle having a noise attenuation device driven by shape memory material actuators

#26
20050126174
2005-06-16

Rotary adjustable exhaust nozzle